Charger connector for an electric aircraft

1. A connector of an electric aircraft charger, the connector comprising:

a housing configured to attach with an electric aircraft port of an electric aircraft to facilitate a charging connection between the charger and the electric aircraft, wherein the housing comprises a fastener for removable attachment with the electric aircraft port, wherein the charging connection comprises an electric communication and a mechanical communication;

a conductor configured to conduct a current of the charging connection;

a control circuit configured to:

receive a control signal from a remote device; and

terminate the charging connection between the charger and the electric aircraft as a function of the control signal, wherein the control circuit is configured to disengage the electric communication to terminate the charging connection between the charger and the electric aircraft, wherein the control circuit is configured to disconnect the mechanical communication of the charging connection between the charger and the electric aircraft by detaching the fastener of the connector from the electric aircraft port.

2. The connector of claim 1 , further comprising a sensor configured to detect a characteristic of the charger.

3. The connector of claim 1 , wherein the conductor is further configured to charge a battery of the electric aircraft.

4. The connector of claim 1 , wherein the conductor comprises a direct current conductor configured to conduct a direct current.

5. The connector of claim 1 , wherein the conductor comprises an alternating current conductor configured to conduct an alternating current.

6. The connector of claim 5 , wherein a direct current conductor and the alternating current conductor are further configured to conduct a communication signal by way of power line communication.

7. The connector of claim 1 , further comprising an electrical sensor communicatively connected to the charging connection and configured to detect the current of the charging connection.

8. The connector of claim 1 , further comprising a proximity signal conductor configured to conduct a proximity signal indicative of attachment with the electric aircraft port when the housing is mated with the electric aircraft port.

9. A method of terminating a charging connection using a connector, the method comprising:

attaching, by a fastener of a housing of the connector, the housing of the connector to an electric aircraft port of an electric aircraft to facilitate a charging connection between the charger and the electric aircraft, wherein the charging connection comprises an electric communication and a mechanical communication;

conducting, by a conductor of the connector, a current of the charging connection;

receiving, by a control circuit of the connector, a control signal from a remote device;

terminating, by the control circuit, the charging connection between the charger and the electric aircraft as a function of the control signal;

disengaging, by the control circuit, the electric communication to terminate the charging connection between the charger and the electric aircraft; and

disconnecting, by the control circuit, the mechanical communication of the charging connection between the charger and the electric aircraft by detaching the fastener of the connector from the electric aircraft port.

10. The method of claim 9 , further comprising detecting, by a sensor, a characteristic of the charger.

11. The method of claim 9 , further comprising charging, by the conductor, a battery of the electric aircraft.

12. The method of claim 9 , wherein the conductor comprises a direct current conductor configured to conduct a direct current.

13. The method of claim 9 , wherein the conductor comprises an alternating current conductor configured to conduct an alternating current.

14. The method of claim 9 , wherein the connector comprises an electrical sensor communicatively connected to the charging connection and configured to detect the current of the charging connection.